2 Patents
- US117397122023Convergent-divergent Flap Pair for a Variable-geometry Turbojet Engine Nozzle, the Flaps of Which Each Comprise a Cooling Air Circulation Duct
SAFRAN AIRCRAFT ENGINES
0 cites - US117137302023Convergent-divergent Flap Pair for a Variable-geometry Turbojet Engine Nozzle Comprising Cooling Air Circulation Ducts Connected Through Contact Surfaces
SAFRAN AIRCRAFT ENGINES
0 cites